# Service difficulty reports: N33202, cancelled Jan 21, 1998

A list on [N33202, cancelled Jan 21, 1998](https://openairdocs.org/deregistered/N33202-1998-01-21.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA9700912](https://openairdocs.org/sdr/CALA9700912.md): Wire Harness · damaged · Jun 17, 1997 · N33202 · Boeing 737130 · APU System Wiring
  > THE APU FIRE LIGHT ILLUMINATED ON SHORT FINAL INTO CLE DURING APU START. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE APU HAD TORCHED ON START RESULTING IN BURN THROUGH OF HARNESS FOR TAILPIPE FIRE DETECTOR. THE APU COMBUSTOR AND T
- [SDR CALA9700066](https://openairdocs.org/sdr/CALA9700066.md): Prox Sensor · inoperative · Jan 16, 1997 · N33202 · Boeing 737130 · Landing Gear Position and Warning
  > THE LEFT MLG RED UNSAFE LIGHT ILLUMINATED AFTER GEAR WAS EXTENDED ON APPROACH. EMERGENCY PROCEDURES WERE COMPLIED WITH PER AIRCRAFT FLIGHT MANUAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG DOWNLOCK PROXIMITY SENSOR AT FAULT. THE
- [SDR CALA9601521](https://openairdocs.org/sdr/CALA9601521.md): Skin · cracked · Oct 23, 1996 · N33202 · Boeing 737130 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CRACKS IN SECTION 41 RT FUSELAGE EXTERNAL SKIN FROM BS 188 TO 251.6, WL 207 TO 234. THE CRACK LENGTHS WERE NOT IDENTIFIED. THE SKIN WAS REPAIRED IAW EA 5310-01188.
- [SDR CALA9601519](https://openairdocs.org/sdr/CALA9601519.md): Fitting · cracked · Oct 23, 1996 · N33202 · Boeing 737130 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN FRAME FITTING AT BS 685, WL 208, LBL 62. THE FASTENER HOLE WAS COLD WORKED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5310-03346.
- [SDR CALA9601517](https://openairdocs.org/sdr/CALA9601517.md): Frame · cracked · Oct 23, 1996 · N33202 · Boeing 737130 · Fuselage Main, Frame
  > INSPECTION FOUND A 2 INCH CRACK EXTENDING AFT OF SECOND FASTENER HOLE IN LT BS 727 FRAME CHORD. THE LOWER CHORD SEGMENT WAS REMOVED AND REPLACED IAW CAL WORK CARD JA5310-0163802001.
- [SDR CALA9601518](https://openairdocs.org/sdr/CALA9601518.md): Floorbeam · cracked · Oct 22, 1996 · N33202 · Boeing 737130 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 1.5 INCH CRACK IN LOWER RADIUS OF FLOORBEAM AT STA 675, BBL 0. THE LOWER T-CHORD WAS REMOVED, A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 51-20-2, 51-30-2 AND BOEING DRAWING NR 65-45410.
- [SDR CALA9601520](https://openairdocs.org/sdr/CALA9601520.md): Skin · cracked · Oct 21, 1996 · N33202 · Boeing 737130 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN RT FUSELAGE SKIN AT BS 747 AND AT BS 727A. BOTH CRACKED AREAS WERE CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED OVER EACH CRACK FROM STA 725 TO 790 IAW SRM 53-30-3.
- [SDR CALA9601516](https://openairdocs.org/sdr/CALA9601516.md): Bulkhead · cracked · Oct 21, 1996 · N33202 · Boeing 737130 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 6 INCH CRACK IN BULKHEAD BEHIND STIFFENER ON RT SIDE AT STA 178, WL 218. ALSO, A 1 INCH CRACK WAS FOUND AT WL 230.5, RT SIDE. THE CRACKED AREA AT WL 218 WAS REMOVED AND THE CRACK AT WL 230.5 WAS STOP DRILLED IAW SRM 53-10-11. REPAIR DOUBL
- [SDR CALA9601423](https://openairdocs.org/sdr/CALA9601423.md): Wire · burned · Oct 7, 1996 · N33202 · Boeing 737130 · Engine Bleed Air System Wiring
  > SMOKE DEVELOPED FROM BEHIND COCKPIT OVERHEAD PANEL AFTER TURNING ON ENGINE ANTI-ICE WHILE CRUISING AT FL 240 EN ROUTE FROM EWR TO CAE. THE SMOKE CEASED WHEN ANTI-ICE WAS TURNED OFF. THE FLIGHT WAS CONTINUED TO CAE WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAI
- [SDR CALA9601017](https://openairdocs.org/sdr/CALA9601017.md): Tire · failed · Jul 13, 1996 · N33202 · Boeing 737130 · Tire
  > A LOUD BANG WAS HEARD AFTER TAKEOFF, WHILE CLIMBING THROUGH 3,000 FEET. THE FLIGHT CONTINUED TO BOS WHERE IT LANDED SAFELY. MAINTENANCE FOUND THAT THE NR 3 TIRE HAD BLOWN RESULTING IN DAMAGE TO RT OUTBOARD SIDE OF WHEEL WELL. THE RT I/B FLAP TRACK FAIRING A
- [SDR CAL960190](https://openairdocs.org/sdr/CAL960190.md): Lamp · inoperative · Feb 25, 1996 · N33202 · Boeing 737130 · Landing Gear Position and Warning
  > FLT NR 591 - MSP - THE RIGHT MLG GREEN LIGHT DID NOT ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH TO MSP, AND IT WOULD NOT TEST. CHANGING BULBS DID NOT HELP. THE GEAR WAS VISUALLY INSPECTED AND CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WI
- [SDR CAL951130](https://openairdocs.org/sdr/CAL951130.md): Stringer · cracked · Nov 22, 1995 · N33202 · Boeing 737130 · Wing, Longeron/Stringer
  > GSO - INSPECTION FOUND A 2 INCH CRACK IN RT WING STR 13 AT WBL 92.5 AND A 1.5 INCH CRACK IN SAME STRINGER AT WBL 114. THE STRINGER WAS REPAIRED IAW BOEING DWG 65C34533. (X)
- [SDR CAL951131](https://openairdocs.org/sdr/CAL951131.md): Chord · cracked · Nov 17, 1995 · N33202 · Boeing 737130 · Fuselage Miscellaneous Structure
  > GSO - INSPECTION FOUND STA 727 RT CHORD CRACKED AT STR 18A. THE CRACK WAS LOCATED AT BOTH FORWARD AND AFT FASTENERS AND TOTALED 1 INCH IN LENGTH. THE CRACKED CHORD SEGMENT WAS REMOVED AND REPLACED IAW EA 5310-01638 AND BOEING DWG 65C33722. (X)
- [SDR CAL951129](https://openairdocs.org/sdr/CAL951129.md): Frame · cracked · Nov 10, 1995 · N33202 · Boeing 737130 · Fuselage Main, Frame
  > GSO - INSPECTION FOUND A.75 INCH CRACK IN FRAME AT STA 440. THE FRAME WAS REMOVED AND REPLACED IAW SRM 53-10-04 AND SRM 51-30-0. (X)
- [SDR CAL950984](https://openairdocs.org/sdr/CAL950984.md): Pcu · leaking · Oct 30, 1995 · N33202 · Boeing 737130 · Aileron Control System
  > FLT NR 1790 - THE B-HYDRAULIC SYSTEM HAD A PARTIAL DROP IN QUANTITY WHILE EN ROUTE TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE FOUND THE B-SYSTEM AILERON PCU LEAKING. THE AILERON PCU WAS REMOVED AND REPLACED IAW MM 27-11-71 AND OPERATIO
- [SDR CAL950294](https://openairdocs.org/sdr/CAL950294.md): Hyd Line · leaking · Apr 18, 1995 · N33202 · Boeing 737130 · Hydraulic System, Main
  > EWR - FLT 1477 - THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON DESCENT INTO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE IN LEFT WING ABOVE LEFT GEAR LEAKING. THE LINE WAS REPLACED US

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N33202' AND deregistration_id = 'N33202-1998-01-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N33202-1998-01-21/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.